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  • session 3

    Title

    Upper Stages, Space Transfer, Entry and Landing Systems

    type

    oral

    Description

    Discussion of existing, planned or new advanced concepts for cargo and human orbital transfer. Includes current and near term transfer, entry and landing systems, sub-systems and technologies for accommodating crew and cargo transfer in space.

    Date

    2011-10-04

    Time

    15:00

    Room

    TS-02

    IPC members
    • Chairman: Dr. Luigi Bussolino, Bussolino and Associates, Italy;

    • Chairman: Mr. Harry A. Cikanek, National Oceanic and Atmospheric Administration (NOAA), United States;

    • Rapporteur: Mr. Kenneth Bruce Morris, Booz Allen Hamilton, United States;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    Fregat upper stage upgrades development status

    20

    confirmed

    Mr. François BARREAU

    Arianespace

    France

    2

    Ares I upper Stage Subsystems Design and Development

    20

    confirmed

    Mr. Harry A. Cikanek

    National Oceanic and Atmospheric Administration (NOAA)

    United States

    3

    3rd stage system for H-III launch vehicle: concept and evaluation

    20

    confirmed

    Mr. Tetsuo Hiraiwa

    Japan Aerospace Exploration Agency (JAXA)

    Japan

    4

    VENUS - Conceptual Design for VEGA New Upper Stage

    20

    confirmed

    Dr. Menko Wisse

    EADS Astrium Space Transportation

    Germany

    5

    Concept Design of High Power Solar Electric Propulsion Vehicles for Human Exploration

    20

    confirmed

    Mr. David Hoffman

    NASA Glenn Research Center

    United States

    6

    Concept study on adding return capability to htv

    20

    confirmed

    Mr. Hiroshi Kawato

    Mitsubishi Heavy Industries, Ltd.

    Japan

    7

    A Personal Airbag System for the Orion Crew Exploration Vehicle

    20

    confirmed

    Mr. Sydney Do

    Massachusetts Institute of Technology (MIT)

    United States

    8

    Using monte carlo simulation for design robustness assessments of winged re-entry vehicles.

    20

    confirmed

    Dr. Farid Gamgami

    OHB System AG-Bremen

    Germany

    9

    Outline of the controlled re-entry system of the h-iib upper stage

    20

    confirmed

    Mr. Kenji Egawa

    Mitsubishi Heavy Industries, Ltd.

    Japan